Full Text Available
Note: Clicking the button above will open the full text document at the original institutional repository in a new window.
It is well-known fact that spacecraft’s electronic components operate in an extreme harsh and varying space environments, beside changing orbit or passing through Van Allan Belts during orbital course results of radiation levels change. This thesis focuses on SRAM-based FPGA systems on-board of such...
| Main Author: | |
|---|---|
| Format: | Thesis |
| Published: |
AUC Knowledge Fountain
2026
|
| Subjects: | |
| Tags: |
No Tags, Be the first to tag this record!
|
| _version_ | 1867613431822024704 |
|---|---|
| access_status_str | Open Access |
| author | Maklad, Yosof Ali Seif El Din Ali |
| author_browse | Maklad, Yosof Ali Seif El Din Ali |
| author_facet | Maklad, Yosof Ali Seif El Din Ali |
| author_sort | Maklad, Yosof Ali Seif El Din Ali |
| collection | Thesis |
| description | It is well-known fact that spacecraft’s electronic components operate in an extreme harsh and varying space environments, beside changing orbit or passing through Van Allan Belts during orbital course results of radiation levels change. This thesis focuses on SRAM-based FPGA systems on-board of such spacecrafts, that are commonly utilized in space applications’ critical applications due to their capabilities and flexibility to reconfigure, since these systems are vulnerable to frequent negative impacts of ionizing radiation, thus inducing soft and hard errors leading to disastrous failures that could jeopardize the entire spacecraft. The soft errors’ effects are frequent yet can be mitigated, specifically SEUs and DEUs, through fault tolerance techniques, which are an essential feature in critical systems. However, this approach relies on redundant components that use finite FPGA resources, so replication is limited. This Thesis proposes multi-die FPGA of different technology nodes to capitalize on reliably older technology while benefits from speed and performance of newer technology dice. Varity of fault tolerance architectures’ designs will be investigated in various scenarios of limited area, as well as resilience to high rate of certain types of event upsets exposure, to identify what changes are required in the common and known technique for achieving comparably elevated reliability. CTMCs utilization for calculating architecture reliability in different placement strategies is essential for maximizing system’s operation lifetime. Several case studies illustrate utilization of these techniques on a Xilinx FPGA, and resulted case-by-case reliability are listed after simulation by SHARPE package tool to support recommendation and conclusion. |
| format | Thesis |
| id | oai:fount.aucegypt.edu:etds-3732 |
| institution | American University in Cairo (Egypt) |
| last_indexed | 2026-06-10T12:35:59.828Z |
| license_str | Not specified — see source repository |
| provenance_str_mv | Harvested via OAI-PMH from AUC Knowledge Fountain — bepress |
| publishDate | 2026 |
| publishDateRange | 2026 |
| publishDateSort | 2026 |
| publisher | AUC Knowledge Fountain |
| publisherStr | AUC Knowledge Fountain |
| record_format | dspace |
| source_str | AUC Knowledge Fountain — bepress |
| spelling | oai:fount.aucegypt.edu:etds-3732 Flexible Fault-Tolerant Multi-Die FPGA-based Architectures for Varying Space Environments Maklad, Yosof Ali Seif El Din Ali It is well-known fact that spacecraft’s electronic components operate in an extreme harsh and varying space environments, beside changing orbit or passing through Van Allan Belts during orbital course results of radiation levels change. This thesis focuses on SRAM-based FPGA systems on-board of such spacecrafts, that are commonly utilized in space applications’ critical applications due to their capabilities and flexibility to reconfigure, since these systems are vulnerable to frequent negative impacts of ionizing radiation, thus inducing soft and hard errors leading to disastrous failures that could jeopardize the entire spacecraft. The soft errors’ effects are frequent yet can be mitigated, specifically SEUs and DEUs, through fault tolerance techniques, which are an essential feature in critical systems. However, this approach relies on redundant components that use finite FPGA resources, so replication is limited. This Thesis proposes multi-die FPGA of different technology nodes to capitalize on reliably older technology while benefits from speed and performance of newer technology dice. Varity of fault tolerance architectures’ designs will be investigated in various scenarios of limited area, as well as resilience to high rate of certain types of event upsets exposure, to identify what changes are required in the common and known technique for achieving comparably elevated reliability. CTMCs utilization for calculating architecture reliability in different placement strategies is essential for maximizing system’s operation lifetime. Several case studies illustrate utilization of these techniques on a Xilinx FPGA, and resulted case-by-case reliability are listed after simulation by SHARPE package tool to support recommendation and conclusion. 2026-02-15T08:00:00Z thesis application/pdf https://fount.aucegypt.edu/etds/2670 https://fount.aucegypt.edu/context/etds/article/3732/viewcontent/yosof_ali_seif_el_din_ali_maklad_thesis.pdf Theses and Dissertations AUC Knowledge Fountain FPGA multi-die space reliability SEU/MEU SEU DEU fault tolerance Markov Digital Circuits Electrical and Electronics Other Aerospace Engineering Other Electrical and Computer Engineering Signal Processing Systems and Communications Systems Engineering and Multidisciplinary Design Optimization |
| spellingShingle | FPGA multi-die space reliability SEU/MEU SEU DEU fault tolerance Markov Digital Circuits Electrical and Electronics Other Aerospace Engineering Other Electrical and Computer Engineering Signal Processing Systems and Communications Systems Engineering and Multidisciplinary Design Optimization Maklad, Yosof Ali Seif El Din Ali Flexible Fault-Tolerant Multi-Die FPGA-based Architectures for Varying Space Environments |
| title | Flexible Fault-Tolerant Multi-Die FPGA-based Architectures for Varying Space Environments |
| title_full | Flexible Fault-Tolerant Multi-Die FPGA-based Architectures for Varying Space Environments |
| title_fullStr | Flexible Fault-Tolerant Multi-Die FPGA-based Architectures for Varying Space Environments |
| title_full_unstemmed | Flexible Fault-Tolerant Multi-Die FPGA-based Architectures for Varying Space Environments |
| title_short | Flexible Fault-Tolerant Multi-Die FPGA-based Architectures for Varying Space Environments |
| title_sort | flexible fault tolerant multi die fpga based architectures for varying space environments |
| topic | FPGA multi-die space reliability SEU/MEU SEU DEU fault tolerance Markov Digital Circuits Electrical and Electronics Other Aerospace Engineering Other Electrical and Computer Engineering Signal Processing Systems and Communications Systems Engineering and Multidisciplinary Design Optimization |
| url | https://fount.aucegypt.edu/etds/2670 https://fount.aucegypt.edu/context/etds/article/3732/viewcontent/yosof_ali_seif_el_din_ali_maklad_thesis.pdf |
| work_keys_str_mv | AT makladyosofaliseifeldinali flexiblefaulttolerantmultidiefpgabasedarchitecturesforvaryingspaceenvironments |